Answer the following questions for an orbit with the following Position and Velocity vectors: (R = 7626I...

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Physics

Answer the following questions for an orbit with the followingPosition and Velocity vectors:

(R = 7626I + 4972J + 806K km, V = 0.626I - 0.690J - 6.160Kkm/s)

1. Determine the size of the size (semimajor axis) of thisorbit.

2. Determine the shape (eccentricity) of this orbit.

3. Determine the inclination of this orbit.

4. Determine the right ascension of the ascending node for thisorbit.

5. Determine the argument of the perigee for this orbit.

6. Determine the true anomaly for this orbit.

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